Invention Grant
- Patent Title: Locking element and turbomachine
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Application No.: US15043643Application Date: 2016-02-15
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Publication No.: US10352178B2Publication Date: 2019-07-16
- Inventor: Werner Humhauser , Hermann Klingels
- Applicant: MTU Aero Engines AG
- Applicant Address: DE Munich
- Assignee: MTU Aero Engines AG
- Current Assignee: MTU Aero Engines AG
- Current Assignee Address: DE Munich
- Agency: Barlow, Josephs & Holmes, Ltd.
- Priority: DE102015203290 20150224
- Main IPC: F01D5/32
- IPC: F01D5/32 ; F01D5/30 ; F04D29/32

Abstract:
A locking element for a row of blades of a turbomachine includes a number of blades that are inserted by their roots in an anchoring groove on the rotor side and are thereby held in the radial direction in form-fitting manner in the anchoring groove. The locking element has a basic body that has a front bearing surface and a back bearing surface for form-fitting with opposite-lying groove surfaces, a front lock projection and a back lock projection for engaging in opposite-lying recesses of the anchoring groove, and a threaded region for interacting with a tightening element. Access to the threaded region for the tightening element is blocked on one side.
Public/Granted literature
- US20160245101A1 LOCKING ELEMENT AND TURBOMACHINE Public/Granted day:2016-08-25
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